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Quasi Area Rule for Heat Addition in Transonic and Supersonic Flight Regimes

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Quasi Area Rule for Heat Addition in Transonic and Supersonic Flight Regimes


Published August 1972
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Body shapes, including axisymmetric and three dimensional, have been developed to minimize wave drag. The von Karman ogive and the area rule are examples. Similar work has not been accomplished for optimum shapes with propulsion. Propulsion can be divided


Publisher Monterey, CA : Naval Postgraduate School
Pages 162
Language en_US
Call number AFAPL-TR-72-10
Digitizing sponsor Naval Postgraduate School, Dudley Knox Library
Book contributor Naval Postgraduate School, Dudley Knox Library
Collection navalpostgraduateschoollibrary; fedlink; americana

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